Faraday current and temperature sensors

ABSTRACT

Techniques and devices for sensing or measuring electric currents and/or temperature based on photonic sensing is disclosed. An optical current sensor head is located near or at a current-carrying conductor so that a magnetic field associated with the current is present at a Faraday material and the optical detection unit detects the light from the Faraday material to determine a magnitude of the current. An optical temperature sensor head is located near or at a location so that the temperature at a temperature-sensing Faraday material is reflected by the optical polarization rotation which is detected to determine the temperature.

PRIORITY CLAIM AND CROSS REFERENCE TO RELATED APPLICATIONS

This patent document is a continuation of and claims priority to U.S.patent application Ser. No. 14/509,015, filed on Oct. 7, 2014, whichclaims the benefit of priority of U.S. Provisional Patent ApplicationNo. 61/887,897 entitled “COMPACT FARADAY CURRENT SENSOR” and filed onOct. 7, 2013. The entire content of the before-mentioned patentapplication is incorporated by reference as part of the disclosure ofthis document.

TECHNICAL FIELD

This patent application relates to techniques and devices for sensing anelectric current and temperature.

BACKGROUND

An electric current is an electrical signal due to flow of charges in anelectrically conductive path such as a metal. Given the electricalnature of the electric currents, techniques and devices for sensing ormeasuring an electric current have been largely based on electroniccircuits. Electronic circuits usually require electrical power and canbe adversely affected by electromagnetic interference. Variouselectronic circuits for sensing currents need to be located at thelocations where the currents are measured and this may impose practicallimitations in various applications.

SUMMARY

This patent application discloses techniques and devices for sensing ormeasuring electric currents and temperature based on photonic sensingtechniques.

In one aspect, a current sensor based on optical sensing is provided toinclude, a sensor base station including a light source that producesprobe light and an optical detection unit; an output fiber line having afirst fiber line terminal coupled to the sensor base station to receivethe probe light from the light source and to direct the received probelight to a second fiber line terminal of the output fiber line away fromthe sensor base station; and an optical current sensor head coupled tothe second fiber line terminal of the output fiber line to receive theprobe light. This head is configured to include an input opticalpolarizer to filter the probe light to produce a polarized input beam, aFaraday material located to receive and transmit the polarized inputbeam as a modified optical beam, and an optical polarization separationdevice that receives the modified optical beam from the Faraday materialand splits the modified optical beam into first and second beams in twodifferent polarizations along first and second optical paths,respectively. This current sensor based on optical sensing furtherincludes a first return fiber line having a first fiber line terminalcoupled to the optical current sensor head to receive the first beam anda second fiber line terminal coupled to the optical detection unit ofthe sensor base station to deliver the first beam from the opticalcurrent sensor to the optical detection unit; and a second return fiberline having a first fiber line terminal coupled to the optical currentsensor head to receive the second beam and a second fiber line terminalcoupled to the optical detection unit of the sensor base station todeliver the second beam from the optical current sensor to the opticaldetection unit. The optical current sensor head is located near or at acurrent-carrying conductor so that a magnetic field associated with thecurrent is present at the Faraday material and the optical detectionunit detects the two optical beams to determine a magnitude of thecurrent.

In another aspect, a current sensor based on optical sensing is providedto include a sensor base station including a light source that producesprobe light and an optical detection unit including a first opticaldetector that receives a portion of the probe light of the light sourceto monitor power fluctuations of the light source and a second opticaldetector that detects light for sensing a current; an output fiber linehaving a first fiber line terminal coupled to the sensor base station toreceive the probe light from the light source and to direct the receivedprobe light to a second fiber line terminal of the output fiber lineaway from the sensor base station; and an optical current sensor headcoupled to the second fiber line terminal of the output fiber line toreceive the probe light. This optical current sensor head is configuredto include an input optical polarizer to filter the probe light toproduce a polarized input beam, a Faraday material located to receiveand transmit the polarized input beam as a modified optical beam, and anoutput optical polarizer that receives the modified optical beam fromthe Faraday material and selectively receives a portion of the modifiedoptical beam as an output beam of the optical current sensor head. Thecurrent sensor based on optical sensing includes a single return fiberline having a first fiber line terminal coupled to the optical currentsensor head to receive output beam and a second fiber line terminalcoupled to the optical detection unit of the sensor base station todeliver the output beam from the optical current sensor to the secondoptical detector inside the optical detection unit. The optical currentsensor head is located near or at a current-carrying conductor so that amagnetic field associated with the current is present at the Faradaymaterial and the second optical detector in the optical detection unitdetects the output beam to determine a magnitude of the current.

In another aspect, a current sensor based on optical sensing is providedto include a sensor base station including a light source that producesprobe light, a first optical detector that receives a portion of theprobe light of the light source to monitor power fluctuations of thelight source and a second optical detector that detects light forsensing a current; an output fiber line having a first fiber lineterminal coupled to the sensor base station to receive the probe lightfrom the light source and to direct the received probe light to a secondfiber line terminal of the output fiber line away from the sensor basestation; and an optical current sensor head coupled to the second fiberline terminal of the output fiber line to receive the probe light. Theoptical current sensor head is configured to include an input opticalpolarizer to filter the probe light to produce a polarized beam, apolarization beam splitter that selectively outputs a first part of thepolarized beam in a first polarization, a Faraday material located toreceive and transmit the first part of the polarized beam in the firstpolarization as a modified optical beam, a polarizer to transmit themodified optical beam and a mirror to reflect the modified optical beamback to the polarizer, the Faraday material and the polarization beamsplitter which outputs the reflected modified optical beam as an outputbeam separated from the probe light received by the optical currentsensor head. The current sensor based on optical sensing includes areturn fiber line having a first fiber line terminal coupled to theoptical current sensor head to receive the output beam to deliver theoutput beam from the optical current sensor to the second opticaldetector in the sensor base station. The optical current sensor head islocated near or at a current-carrying conductor so that a magnetic fieldassociated with the current is present at the Faraday material and thesecond optical detector detects the output beam to determine a magnitudeof the current.

In another aspect, a temperature sensor based on optical sensingincludes a sensor base station including a light source that producesprobe light and an optical detection unit that detects light received bysensor base station; an output fiber line having a first fiber lineterminal coupled to the sensor base station to receive the probe lightfrom the light source and to direct the received probe light to a secondfiber line terminal of the output fiber line away from the sensor basestation; an optical temperature sensor head coupled to the second fiberline terminal of the output fiber line to receive the probe light andconfigured to include an input optical polarizer to filter the probelight to produce a polarized input beam, a Faraday material located toreceive and transmit the polarized input beam as a modified opticalbeam, and an optical polarization separation device that receives themodified optical beam from the Faraday material and splits the modifiedoptical beam into first and second beams in two different polarizationsalong first and second optical paths, respectively; a first return fiberline having a first fiber line terminal coupled to the opticaltemperature sensor head to receive the first beam and a second fiberline terminal coupled to the optical detection unit of the sensor basestation to deliver the first beam from the optical temperature sensor tothe optical detection unit; and a second return fiber line having afirst fiber line terminal coupled to the optical temperature sensor headto receive the second beam and a second fiber line terminal coupled tothe optical detection unit of the sensor base station to deliver thesecond beam from the optical temperature sensor to the optical detectionunit. The Faraday material in the optical temperature sensor head causesa rotation of polarization of light based on a temperature at theFaraday material and the optical detection unit measures the two opticalbeams to determine the temperature.

In yet another aspect, a temperature sensor based on optical sensingincludes a sensor base station including a light source that producesprobe light and an optical detection unit including a first opticaldetector that receives a portion of the probe light of the light sourceto monitor power fluctuations of the light source and a second opticaldetector that detects light received by the sensor base station; anoutput fiber line having a first fiber line terminal coupled to thesensor base station to receive the probe light from the light source andto direct the received probe light to a second fiber line terminal ofthe output fiber line away from the sensor base station; an opticaltemperature sensor head coupled to the second fiber line terminal of theoutput fiber line to receive the probe light and configured to includean input optical polarizer to filter the probe light to produce apolarized input beam, a Faraday material located to receive and transmitthe polarized input beam as a modified optical beam, and an outputoptical polarizer that receives the modified optical beam from theFaraday material and selectively receives a portion of the modifiedoptical beam as an output beam of the optical current sensor head; and asingle return fiber line having a first fiber line terminal coupled tothe optical temperature sensor head to receive output beam and a secondfiber line terminal coupled to the optical detection unit of the sensorbase station to deliver the output beam from the optical current sensorto the second optical detector inside the optical detection unit. TheFaraday material in the optical temperature sensor head causes arotation of polarization of light based on a temperature at the Faradaymaterial and the optical detection unit detects the output beam tomeasure the temperature. In implementations, the optical temperaturesensor is configured to magnetically shield the Faraday material from anexternal magnetic field.

The above and other aspects and their implementations and examples aredescribed in greater detail in the drawings, the description and theclaims.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 shows an example of a first design of a current sensing systembased on the disclosed technology showing a transmissive current sensorhaving a current sensor base station and a remote current sensor head. AWollaston prism is used to separate the two orthogonal polarizationcomponents into two separate fibers. The polarizer is oriented 45degrees from the Wollaston prism to allow 50% splitting when no magneticfield applied. A balanced detector in FIG. 2 can be used to receive thedetected optical power. A variable optical attenuator is used to ensurethat the photocurrent in the two PDs are equal.

FIG. 2 shows an example of an optical detection circuit using twoseparate photodetectors to detect the optical power levels from the twooutput fibers in FIG. 1.

FIG. 3 shows another example of an optical detection circuit in abalanced detection design to detect the differential power levels fromthe two output fibers in order to significantly increase the detectionsensitivity or the dynamic range of the current sensor system in FIG. 1.

FIG. 4 shows an example of a temperature sensor with the sameconstruction as the current sensor in FIG. 1, where the variable Faradayrotator in FIG. 1 is replaced with the permanent Faraday rotator of xdegrees, which is magnetically shielded to prevent the influence of thecurrent to be sensed.

FIG. 5 shows an example of a simpler embodiment of the temperaturesensor based on the permanent Faraday rotator, in which the Wollastonprism in FIG. 4 is replaced with a polarizer (polarizer 2) and the dualfiber collimator is replaced with a single fiber collimator.

FIG. 6 illustrates an example of a first embodiment of combining acurrent sensor head and a temperature sensor head into a same package.

FIG. 7 illustrates an example of a second embodiment of combining acurrent sensor head and a temperature sensor head into a same package.

FIG. 8 shows an example of a transmissive current sensor with built-intemperature sensing capability, where a permanent Faraday rotator withan x degree rotation as in FIGS. 6 and 7 is placed in front of thesensing Faraday rotator.

FIG. 9 shows an example of a first embodiment of a reflective currentsensor head, in which the polarizer is oriented 45 degrees from the PBSpassing axis so that the reflected light from the mirror is split 50% bythe PBS into two separate fibers at zero magnetic field.

FIGS. 10, 11 and 12 show examples of a reflective current sensor headwith an integrated temperature sensing capability.

FIG. 13 shows an example of a current sensing system for simultaneouslymonitoring currents in three conductors in a 3-phase power system.

DETAILED DESCRIPTION

Sensing of an electric current based on a fiber optic current sensor isattractive for monitoring, control, and protection of substations andpower distribution systems in smart grid. Comparing with some existingcurrent sensors, they have the advantage of being able to separate thesensor head and electronic processing unit at different locations, andtherefore do not require any electrical power at the sensor head, makingit safe for high voltage applications. Implementations of fiber opticcurrent sensors can be configured to achieve other advantages, includingsmall size, light weight, immune to electromagnetic interferences, lowpower consumption, immunity to current saturation or others. Fiber coilbased current sensors using Faraday effect in the fiber have been widelyused for high-voltage applications where the fiber coil winds around thecurrent-carrying conductor. Such fiber coil based current sensors aregenerally more expensive and require breaking an electrical cable toinstall. Fiber current sensors based on Faraday glasses or crystals havethe advantages of compact size, light weight, low cost, and easyinstallation, compared with their fiber coil based counterparts. Inparticular, they can directly mount on the current conducting cable evenwith life current flow, and can significantly reduce the installationcost. Because of the low cost and small size, they can be applied to lowand medium voltage applications for transformer monitoring, andtherefore have a much larger market potential.

Accuracy, dynamic range, and environmental stability are the mainperformance indicators for the fiber optic current sensors. An effectiveway to increase the dynamic range is to increase the magnetic fielddetection sensitivity, requiring significantly reducing the noise inoptoelectronics detection circuitry. The temperature dependence of theVerdet constants of the Faraday glasses or crystals poses challenges forthe for the measurement accuracy and need to be addressed in the sensorsystems design. The temperature effect on the optical signal derivedfrom the sensor head can impact the environmentally stable operation ofthe sensor, and thus it is advantageous to provide a mechanism forcompensating for the temperature effect. In addition, interferences ofthe magnetic fields from the neighboring current carrying conductors canalso affect the current detection accuracy, and thus should be reducedor minimized.

This patent document discloses examples of constructions for increasingthe circuit detection sensitivity, measuring the temperature of thesensor head, compensating the temperature effects of the sensor head,and eliminate the interferences from the neighboring conductors forachieving a current sensor system with high accuracy, large dynamicrange, and high environmental stability.

In some implementations, a current sensor based optical sensingdisclosed herein includes a sensor base station including a light sourcethat produces probe light and an optical detection unit, and an opticalcurrent sensor head for sensing the current. The optical current sensoris located away from the current sensor base station and is free ofelectronics. The current sensor includes an output fiber line having afirst fiber line terminal coupled to the sensor base station to receivethe probe light from the light source and to direct the received probelight to a second fiber line terminal of the output fiber line away fromthe sensor base station. The optical current sensor head is coupled tothe second fiber line terminal of the output fiber line to receive theprobe light. The optical current sensor is configured to include aninput optical polarizer to filter the probe light to produce a polarizedinput beam, a Faraday material located to receive and transmit thepolarized input beam as a modified optical beam, and an opticalpolarization separation device that receives the modified optical beamfrom the Faraday material and splits the modified optical beam intofirst and second beams in two different polarizations along first andsecond optical paths, respectively. Included in the current sensor are afirst return fiber line having a first fiber line terminal coupled tothe optical current sensor head to receive the first beam and a secondfiber line terminal coupled to the optical detection unit of the sensorbase station to deliver the first beam from the optical current sensorto the optical detection unit; and a second return fiber line having afirst fiber line terminal coupled to the optical current sensor head toreceive the second beam and a second fiber line terminal coupled to theoptical detection unit of the sensor base station to deliver the secondbeam from the optical current sensor to the optical detection unit. Theoptical current sensor head is located near or at a current-carryingconductor so that a magnetic field associated with the current ispresent at the Faraday material and the optical detection unit detectsthe two optical beams to determine a magnitude of the current.

FIG. 1 shows an example of a first design of a current sensing system. Abroad bandwidth light source with a low degree of polarization (DOP),such as an amplified spontaneous emission (ASE) light source or asuperluminescent light emitting diode (SLED) light source, is used asthe light source to produce the probe light for sensing the current.This use of a light source with a low degree of polarization and abroadband width can be beneficial in various ways. The broad bandwidthlight source is included along with a photodiode (PD) detection unit ina current sensor base station which is linked via fiber to a currentsensor head that is located at a different location away from thecurrent sensor base station having the light source and the photodiodedetection unit. The current sensor head is an all optical current sensorhead formed by optical components without local electronic circuits orcomponents. In this regard, the sensor head does not include any opticaldetector and directs light carrying the measurement information of thecurrent to the current sensor base station via a fiber link. Theall-optical current sensor head is placed by the current-carryingconductor to sense the current based on the optical polarizationrotation caused by the magnetic field associated with the current in theFaraday material inside the all-optical current sensor. When the currentto be measured is perpendicular to the light propagation path of theFaraday rotator, the magnetic field produced by the current is along thelight propagation path of the Faraday rotator and thus exerts mostinfluence to the polarization rotation of the light. The probe lightfrom the broad bandwidth light source is directed to the current sensorhead and a returned light beam is directed back from the current sensorhead back to the photodiode (PD) detection unit within the currentsensor base station via fiber and is detected to extract information onthe electric current sensed by the current sensor head. The low DOPproperty of the probe light is to assure the optical power stabilitypassing through the sensor head if single mode fiber (SMF) or multimodefiber (MMF) is used to deliver light into the sensor head locatedremotely at the current sensing site. If a more expensive polarizationmaintaining (PM) fiber is used, a light source with high DOP can be usedand the polarization axis of the probe light is aligned with the slow(or fast) axis of the PM fiber.

The current sensor head includes an optical polarizer to receive theprobe light from the light source, a Faraday rotator to receive theoutput light from the optical polarizer, and an optical polarizationseparation unit that separates two light beams of two orthogonalpolarizations in the light from the Faraday rotator. The probe lightfirst passes through the polarizer to define the input polarization tothe current sensor head. An input optical collimator may be used tocollimate the light to be directed into the optical polarizer. In animplementation using a low DOP source, there is no requirement of theorientation of the polarizer with respect to the input light. On theother hand, in an implementation based on a PM fiber, the polarizer'spassing axis should be aligned to the slow (or fast) axis of the PMfiber. After the polarizer, the linearly polarized light passes througha Faraday material as the Faraday rotator, such as a length of glass, alength of Faraday crystal, or piece of Faraday film capable of rotatingthe polarization of light in response to a magnetic field parallel tothe Faraday material. The optical polarization separation unit thatreceives output light from the Faraday rotator can be implemented invarious configurations. For example, in FIG. 1, a micro Wollaston prismis used as such an optical polarization separation unit to separate theinput linear polarization into two orthogonal polarization componentspropagating at a small crossing angle, e.g., about 3.7 degrees. Theorientation of the optical polarization direction of the Wollaston prismcan be set to be 45 degrees from the polarizer's passing axis such thatwhen there is no magnetic field present, the two orthogonal polarizationcomponents have equal powers (50% splitting). A dual fiber collimatorwith a crossing angle similar to that of the Wollaston prism is thenused to focus the two polarization components into two separate outputfibers. The two output fibers can be either single mode (SM) fiber ormultimode (MM) fiber to transmit the light back to the current sensorbase station.

The current sensor base station which houses the light source in theexample in FIG. 1 is coupled to the two output fibers to receive thelight from the two fibers in the two polarizations and contains opticalsensing unit that detects and converts the received optical signal sintwo polarizations into two detector signals to be processed by a signalprocessing unit that is remotely located from the current sensor head.Two optical detectors, PD1 and PD2, can be included within the currentsensor base station to detect the returned light in the two fibers fromthe current sensor head, respectively. An optical attenuator, such as avoltage controlled optical attenuator (VOA), may be used to control therelative amplitudes of light received at PD1 and PD2 so that the opticalpower levels of received light in the two fibers are equal when there isno magnetic field present at the remote current sensor head.

The above example in FIG. 1 provides a particular structural design of acurrent sensor based on optical sensing. This current sensor designincludes a sensor base station including a light source that producesprobe light and an optical detection unit; an output fiber line having afirst fiber line terminal coupled to the sensor base station to receivethe probe light from the light source and to direct the received probelight to a second fiber line terminal of the output fiber line away fromthe sensor base station; and an optical current sensor head coupled tothe second fiber line terminal of the output fiber line to receive theprobe light. The head is configured to include an input opticalpolarizer to filter the probe light to produce a polarized input beam, aFaraday material located to receive and transmit the polarized inputbeam as a modified optical beam, and an optical polarization separationdevice that receives the modified optical beam from the Faraday materialand splits the modified optical beam into first and second beams in twodifferent polarizations along first and second optical paths,respectively. In addition, this current sensor based on optical sensingfurther includes a first return fiber line having a first fiber lineterminal coupled to the optical current sensor head to receive the firstbeam and a second fiber line terminal coupled to the optical detectionunit of the sensor base station to deliver the first beam from theoptical current sensor to the optical detection unit; and a secondreturn fiber line having a first fiber line terminal coupled to theoptical current sensor head to receive the second beam and a secondfiber line terminal coupled to the optical detection unit of the sensorbase station to deliver the second beam from the optical current sensorto the optical detection unit. The optical current sensor head islocated near or at a current-carrying conductor so that a magnetic fieldassociated with the current is present at the Faraday material and theoptical detection unit detects the two optical beams to determine amagnitude of the current.

In implementations, it is desirable to achieve high detectionsensitivity to provide sensitive and accurate measurements of thecurrent. The two optical detectors can be electrically coupled to oneanother in a balanced detection configuration to reduce noise and toenhance the detection sensitivity.

FIG. 2 shows an example of an optical detection circuit using twoseparate photodetectors PD1 and PD2 to detect the optical powers fromthe two output fibers.

FIG. 3 shows an example of an optical detection circuit in a balanceddetection design to detect the differential power levels from the twooutput fibers in order to significantly increase the detectionsensitivity or the dynamic range of the current sensor system. The useof low DOP light is an important aspect in this implementation. If thelight source has a high DOP, an optical depolarizer can be placed in theoptical path between the light source and the optical sensing head andis used to convert the light with a high DOP into light with asufficiently low DOP, e.g., less than 10%. The use of the balanceddetection can achieve high detection sensitivity.

The electric field of the optical beam after the input polarizer can bewritten as:

=E ₀ ŷ,  (1)where ŷ is the passing axis of the input polarizer. After passingthrough the Faraday rotator with a rotation angle of θ, the electricfield becomes:

=E ₀(cos θ{circumflex over (y)}+sin θ{circumflex over (x)})  (2)

The two principle axes of the Wollaston prism can be represented as:

$\begin{matrix}{{{\hat{w}}_{1} = {\frac{1}{\sqrt{2}}\left( {\hat{y} + \hat{x}} \right)}},{{\hat{w}}_{2} = {\frac{1}{\sqrt{2}}\left( {\hat{y} - \hat{x}} \right)}}} & (3)\end{matrix}$where a relative orientation of 45 degree between the input polarizerand the Wollaston prism is assumed. The powers of the two polarizationcomponents in the two output fibers are therefore:

$\begin{matrix}{{P_{1} = {{\alpha_{1}{{\cdot {\hat{w}}_{1}}}^{2}} = {\frac{\alpha_{1}E_{0}^{2}}{2}\left( {1 + {\sin\; 2\;\theta}} \right)}}},} & (4) \\{P_{2} = {{\alpha_{2}{{\cdot {\hat{w}}_{2}}}^{2}} = {\frac{\alpha_{2}E_{0}^{2}}{2}\left( {1 - {\sin\; 2\;\theta}} \right)}}} & (5)\end{matrix}$where α₁ and α₂ are the optical losses caused by the coupling andimperfections of the optical parts. The photocurrent received by the twoPDs are therefore:

$\begin{matrix}{I_{1} = {{\frac{\rho_{1}\alpha_{1}E_{0}^{2}}{2}\left( {1 + {\sin\; 2\;\theta}} \right)} = {I_{10}\left( {1 + {\sin\; 2\;\theta}} \right)}}} & (6) \\{{I_{2} = {{\frac{\rho_{1}\alpha_{2}E_{0}^{2}}{2}\left( {1 - {\sin\; 2\;\theta}} \right)} = {I_{20}\left( {1 - {\sin\; 2\;\theta}} \right)}}},} & (7)\end{matrix}$where ρ₁ and ρ₂ are responsivities of PD1 and PD2 respectively, and I₁₀and I₂₀ are the nominal photocurrent in PD1 and PD2 respectively.

If the signals from the two PDs are separately amplified, as in FIG. 2,the gains of the two amplifiers may be adjusted or set to obtain:V ₁ =V ₀(1+sin 2θ)  (8)V ₂ =V ₀(1−sin 2θ),  (9)where V₀=ρ₁α₁G₁E₀ ²/2=ρ₂α₂G₂E₀ ²/2, and G₁ and G₂ are thetrans-impedance gains of PD1 and PD2, respectively.

$\begin{matrix}{{\sin\; 2\;\theta} = \frac{V_{1} - V_{2}}{V_{1} + V_{2}}} & (10)\end{matrix}$

The power fluctuations of the light source can be eliminated with thedouble outputs.

In some of the prior art current sensors designs, only a singlephotodetector is used and the corresponding photovoltage can still beexpressed in Eq. (8). Because the conductor current is AC with afrequency of 50 or 60 Hz, Eq. (8) can be separated into DC and ACcomponents: V_(DC)=V₀ and V_(AC)=V₀ sin 2θ. The Faraday rotation anglecan be obtained by sin 2θ=V_(AC)/V_(DC). In practical circuits, the ACand DC components of a signal can easily be separated using a bias teeor high-pass and low-pass filters.

The optical attenuation or the electrical circuits may be controlledsuch that ρ₁α₁=ρ₂α₂=ρα to obtain:I ₁ =I ₀(1+sin 2θ)  (11)I ₂ =I ₀(1−sin 2θ)  (12)where I₀=ραE₀ ²/2. Using the balanced detection circuitry as in FIG. 3,the relation between the differential photo current and the Faradayrotation angle can be represented by:

$\begin{matrix}{{\sin\; 2\;\theta} = \frac{\left( {I_{1} - I_{2}} \right)}{\left( {I_{1} + I_{2}} \right)}} & (13)\end{matrix}$

Although Eq. (10) for FIG. 2 and Eq. (13) for FIG. 3 may look similar,the circuitry of FIG. 3 has much better detection sensitivity anddynamic range than the circuitry of FIG. 2.

In general, the current induced rotation angle can be expressed as:θ(j,T)=θ₀(T)+V _(d)(T)·j(t)·L=θ ₀(T)+j(t)  (14)where θ₀(T) is a rotation bias, j(t) is the electrical current in theconductor and β(T)=V_(d)(T)L, with V_(d)(T) and L being the Verdetconstant (temperature sensitive) and the length of the Faraday materialrespectively. In power generation and distribution systems, theconductor current is generally AC with a frequency of 50 or 60 Hz, andcan be expressed as:j(t)=j _(dc) +j _(ac) sin(ωt+ϕ ₀)  (15)where j_(dc) is the residual DC component of the current, j_(ac), ω, andϕ₀ are the amplitude, angular frequency and the phase of the ACcomponent of the current in the conductor, respectively. When the powerstation is normal, the DC component should be close to zero. However,when the power station operates abnormally, DC component will benon-zero.θ(I,T)=γ(T)+β(T)j _(ac) sin(ωt+ϕ ₀)  (16)whereγ(T)=θ₀(T)+β(T)j _(dc)  (17)is the DC term of the rotation angle. Eq. (15) can be substituted in Eq.(11) and Eq. (12) to obtain the following:

$\begin{matrix}{{I_{1}(t)} = {I_{0}\left\{ {1 + {\sin\;{2\left\lbrack {{\gamma(T)} + {{\beta(T)}j_{ac}{\sin\left( {{\omega\; t} + \phi_{0}} \right)}}} \right\rbrack}}} \right\}}} & (18) \\{{I_{2}(t)} = {I_{0}\left\{ {1 - {\sin\;{2\left\lbrack {{\gamma(T)} + {{\beta(T)}j_{ac}{\sin\left( {{\omega\; t} + \phi_{0}} \right)}}} \right\rbrack}}} \right\}}} & (19) \\{{\Delta\;{I_{12}(t)}} = {{{I_{1}(t)} - {I_{2}(t)}} = {2\; I_{0}\sin\;{2\left\lbrack {{\gamma(T)} + {{\beta(T)}j_{ac}{\sin\left( {{\omega\; t} + \phi_{0}} \right)}}} \right\rbrack}}}} & \left( {20\; a} \right) \\{{\Delta\;{I_{12}(t)}} \approx {4\; I_{0}{\beta(T)}j_{ac}{\sin\left( {{\omega\; t} + \phi_{0}} \right)}}} & \left( {20\; b} \right) \\{{j(t)} = {{j_{ac}{\sin\left( {{\omega\; t} + \phi_{0}} \right)}} \approx \frac{\Delta\;{I_{12}(t)}}{{4\left\lbrack {{I_{1}(t)} + {I_{2}(t)}} \right\rbrack}{{LV}_{d}(T)}}}} & \left( {20\; c} \right)\end{matrix}$In Eq. (20b) and (20c), β(T)j_(ac)<<1 and γ(T)=0 are assumed. Eq. (18)and Eq. (19) can be expanded using Bassel functions:

$\begin{matrix}{{\Delta\;{I_{12}(t)}} = {\quad{2\; I_{0}\left\{ {{\sin\; 2\;\gamma\;{J_{0}\left( {2\;\beta\; j_{ac}} \right)}} + {\cos\; 2\;\gamma\;{\sum\limits_{1}^{\infty}{{J_{{2\; m} - 1}\left( {2\;\beta\; j_{ac}} \right)}{\sin\left\lbrack {\left( {{2\; m} - 1} \right)\left( {{\omega\; t} + \phi_{0}} \right)} \right\rbrack}}}} + {\sin\; 2\;\gamma\;{\sum\limits_{1}^{\infty}{{J_{2\; m}\left( {2\;\beta\; j_{ac}} \right)}{\cos\left\lbrack {2\;{m\left( {{\omega\; t} + \phi_{0}} \right)}} \right\rbrack}}}}} \right\}}}} & (21)\end{matrix}$

For the DC term:ΔI ₁₂(DC)=2I ₀ sin 2γI ₀(2βj _(ac))  (22)

For the ω term:ΔI ₁₂(ω)=2I ₀ cos 2γJ ₁(2βj _(ac))  (23)

For the 2 ω term:ΔI ₁₂(2ω)=2I ₀ sin 2γJ ₂(2βj _(ac))  (24)

For the nω term:ΔI ₁₂(nω)=2I ₀ sin 2γJ ₂(2βj _(ac)),n is even  (25a)ΔI ₁₂(n(nω)=2I ₀ cos 2γJ _(n)(2βj _(ac)),n is odd  (25b)

The output from the balanced detector of FIG. 3 can be separated into aDC and AC parts. The DC part is represented by Eq. (32) and the Fouriercomponents of the AC parts are represented by Eqs. (23), (24), and (25),and they can be obtained by taking FFT of the AC part of the signalafter A/D converter. The digital filtering of each Fourier component canbe used to increase the signal to noise ratio. Referring to FIG. 3,ΔI₁₂(t), I₁(t), and I₂ (t) can be obtained by:ΔI ₁₂(t)=V ₁₂ /G ₁₂  (26)I ₁(t)=V ₁ /G ₁  (27)I ₂(t)=V ₂ /G ₂,  (28)where G₁₂, G₁, and G₂ are the trans-impedance gains of the operationamplifiers for the three photocurrents, respectively.I ₀ =I ₁(t)+I ₂(t)  (29)

The peak detection of the AC part of the differential signal ΔI₁₂ (t)can be used to obtain the maximum current in the conductor from Eq.(20b):j _(ac) ≈ΔI ₁₂(peak)/(4I ₀β),  (30)where γ<<1 and βj_(ac)<<1 are assumed in Eq. (20).

Such a peak current detection is fast (instantaneous) but with a lessaccuracy. The result can be used for circuit protection purpose. For,signal processing by using the Fourier components can be used to achievehigh accuracy measurements.

In an ideal case, γ=0 (no DC component in the conductor current and norotation angle bias), ΔI₁₂ (ω) and I₀ can be determined by using Eq.(23) and Eq. (29), and the value of β(T) j_(ac) can be determined byusing a look up table. In the case of malfunctioning, the DC componentmay not be zero and the relative relationship among harmonic componentsof the differential current can change. In this case, Eq. (23) can beused to obtain β(T)j_(ac) by assuming γ=0. The value of γ can beobtained by substituting β(T)j_(ac) into Eq. (22). The obtained γ can beput into Eq. (23) to obtain more accurate β(T) j_(ac), and a moreaccurate measurement of γ can be obtained using Eq. (22). The aboveprocess can be repeated until both γ and β(T) j_(ac) converge.

In implementations, both γ and β(T) may be temperature dependent and theaccuracy of the final obtained current amplitudes j_(ac) and j_(dc) areaffected by the temperature change. One way to solve the problem is tofind a way to measure the temperature at the sensor and find theaccurate value of β(T) and γ at the corresponding temperature. For thispurpose, the precise temperature dependences of γ and β(T) can bedetermined with a calibration procedure by using the fiber optic sensorto measure a known current (measured with a standard current measurementinstrument) at different temperature settings and obtain measurements ofcurves of β(T) vs. T and γ vs. T. The linear fit of the curves can yieldthe temperature coefficients of both γ and β(T). In obtaining thetemperature dependence of γ, j_(dc) is assumed to be zero. Only therotation angle bias θ₀ (T) is considered.

The optical sensing for measuring currents in FIG. 1 can be configuredto for measuring temperature. FIGS. 4 and 5 show two examples of such atemperature sensor.

FIG. 4 discloses a temperature sensor with the same construction as thecurrent sensor in FIG. 1, where the variable Faraday rotator in FIG. 1is replaced with the permanent Faraday rotator of a particular amount ofpolarization rotation at a rotation angle of some specific degrees. Thepermanent Faraday rotator includes a transparent Faraday material and amagnetic structure to produce a magnetic field along the propagationpath of the light in the transparent Faraday material. The permanentFaraday rotator is magnetically shielded from influence of any externalmagnetic field, preventing the influence of the magnetic field from acurrent such as the current to be sensed. The polarization rotationangle produced by the Faraday material varies with the temperature ofthe material and this dependence of the rotation with the temperature,when the material is free of an external magnetic field along the lightpropagation direction, can be used to measure the temperature at thematerial. The Wollaston prism is oriented to allow equal power splittinginto the two output fibers at the room temperature during the assemblyof the sensor head. In implementations, the permanent Faraday rotatormay be set at a nominal rotation angle of 45° (x=45°). The rotationangle of the rotator will vary due to the temperature dependenceinherent of the permanent Faraday rotator. The temperature inducedrotation angle variation will cause the photocurrents detected in PD1and PD2 to vary, which have the similar to those of Eq. (11)-Eq. (12):I ₁ =I ₀[1+sin 2θ(T)],  (31)I ₂ =I ₀[1−sin 2θ(T)],  (32)θ(T)=a(T−T ₀)  (33)

Hence a temperature dependence of the power difference can be obtainedand be used to calculate the temperature. The temperature sensor can beco-located with the current sensor in FIG. 1 to detect the temperatureat the current sensor for correcting any errors caused by thetemperature sensitivity of the Faraday material in the current sensor.The parameters a and T₀ of in θ(T) of a temperature sensor can beobtained for each temperature sensor by putting the sensor in atemperature chamber with different temperature settings. Therefore, thetemperature can be obtained using:

$\begin{matrix}{T = {\frac{\left( {I_{1} - I_{2}} \right)}{4\;{a\left( {I_{1} + I_{2}} \right)}} + T_{0}}} & (34)\end{matrix}$

FIG. 5 discloses a simpler embodiment of the temperature sensor based onthe permanent Faraday rotator, in which the Wollaston prism in FIG. 4 isreplaced with a polarizer (polarizer 2) and the dual fiber collimator isreplaced with a single fiber collimator. Polarizer 2 is oriented either0° or 90° nominally from polarizer 1. The permanent Faraday rotator canbe set at a nominal rotation angle, e.g., in 45° in someimplementations. The rotation angle will be varied due to thetemperature dependence inherent of the permanent Faraday rotator. Thetemperature induced rotation angle variation will cause the powerdetected in PD2 to vary and hence a temperature dependence of the powercan be obtained and be used to calculate the temperature. The optionalPD1 is used to monitor the power fluctuation of the light source and toremove the effect of the power fluctuation.

The example in FIG. 5 illustrates another design for a current sensorbased on optical sensing. Under this design, a current sensor includes asensor base station including a light source that produces probe lightand an optical detection unit including a first optical detector thatreceives a portion of the probe light of the light source to monitorpower fluctuations of the light source and a second optical detectorthat detects light for sensing a current; an output fiber line having afirst fiber line terminal coupled to the sensor base station to receivethe probe light from the light source and to direct the received probelight to a second fiber line terminal of the output fiber line away fromthe sensor base station; and an optical current sensor head coupled tothe second fiber line terminal of the output fiber line to receive theprobe light. This optical current sensor head is configured to includean input optical polarizer to filter the probe light to produce apolarized input beam, a Faraday material located to receive and transmitthe polarized input beam as a modified optical beam, and an outputoptical polarizer that receives the modified optical beam from theFaraday material and selectively receives a portion of the modifiedoptical beam as an output beam of the optical current sensor head. Thecurrent sensor based on optical sensing includes a single return fiberline having a first fiber line terminal coupled to the optical currentsensor head to receive output beam and a second fiber line terminalcoupled to the optical detection unit of the sensor base station todeliver the output beam from the optical current sensor to the secondoptical detector inside the optical detection unit. The optical currentsensor head is located near or at a current-carrying conductor so that amagnetic field associated with the current is present at the Faradaymaterial and the second optical detector in the optical detection unitdetects the output beam to determine a magnitude of the current.

FIG. 6 illustrates a first embodiment of combining a current sensor headand a temperature sensor head into a same package. A 10% coupler may beused to direct a small portion of the light into the temperature sensorhead as the light source.

FIG. 7 illustrates a second embodiment of combining a current sensorhead and a temperature sensor head into a same package. The temperaturesensing permanent Faraday rotator is oriented 90 degrees from thecurrent sensing Faraday rotator so that the magnetic field induced bythe conductor current has no effect on the permanent Faraday rotatoreven without magnetic shield around the permanent Faraday rotator.

In both FIGS. 6 and 7, the combination of current and the temperaturesensors allow the temperature measurement by the temperature sensoroutput to be used for compensate for the temperature dependency in thecurrent measurement obtained by the current sensor since thepolarization rotation in the Faraday material in the current sensorvaries with the temperature. This temperature-calibrated measurement canbe performed by the sensor base station where the effect of thetemperature-induced polarization rotation of the probe light in theFaraday material for current sensing is calibrated by the effect of thetemperature-induced polarization rotation measured in the other Faradaymaterial for measuring the temperature. The sensor base station isstructured to use a temperature measurement by the third opticaldetector to compensate for a temperature-induced effect to themeasurement of the current. In these configurations, the current sensorand temperature sensor are separated from one another and operate basedon separate light beams.

FIG. 8 discloses a transmissive current sensor with built-in temperaturesensing capability. Two Faraday rotators are used in this design where apermanent Faraday rotator with a desired amount of polarization rotationas in FIGS. 6 and 7 is configured a temperature sensor and is placed inthe front of a second Faraday rotator that is configured as a currentsensing Faraday rotator. The current sensor and temperature sensor areoptically connected to the same probe light path in series to reduce thestructure complexity and to reduce cost of the device. The DC portion ofthe output optical signal from the sensor head is proportional to thetemperature values while the AC portion is proportional to currentvalues, assuming the current to be sensed is an AC current. A Wollastonprism is used to separate the two orthogonal polarization componentsinto two separate fibers. The polarizer is oriented x+45 degrees fromthe Wollaston prism to allow 50% splitting when no magnetic fieldapplied. A balanced detector in FIG. 3 can be used to receive thedetected optical power. A magnetic shield may be used around thepermanent Faraday rotator to prevent the influence of the current to besensed to affect the temperature sensing. Any other material withtemperature induced polarization change, such as a waveplate can also beused in the place of the permanent Faraday rotator for sensing thetemperature. The photocurrents received in PD1 and PD2 can also beexpressed with Eqs. (11) and (12) or Eqs. (18) and (19), where therotation bias θ₀(T) in Eq. (24) is adjusted to be 0 at room temperatureby optical alignment during the assembly process (corresponding to equalsplitting of the powers in two output fibers). When temperature deviatefrom the room temperature, θ₀(T) will change and may follow a polynomialrelation:θ₀(T)=a(T−T ₀)+b(T−T ₀)² +c(T−T ₀)³  (35)where the coefficients a, b, and c can be obtained during a calibrationprocess by changing the environment temperature of the sensor in theabsence of any magnetic field (no conductor current). In fact, a linearrelationship is expected for ideal cases and the coefficients b and care expected to be negligible.

When the power generation and distribution system is in normaloperation, the currents in the system are AC currents and no DC currentis expected in the conductor. The parameter γ is solely determined byθ₀(T) from Eq. (17):γ(T)=θ₀(T)  (36)

Therefore when γ(T) is obtained using Eqs (23) and (22) iteratively asdescribed previously, θ₀(T) is automatically obtained, and thecorresponding temperature can be obtained using Eq. (31). When thetemperature is known, the correct Verdet constant at the temperature canbe used and the accurate conductor current can be obtained whenβ(T)j_(ac)=V_(d)(T)Lj_(ac) is obtained using Eqs. (23) and (22)iteratively. Because the malfunctioning of power system occurs veryfast, the DC component of the conductor current may have a sudden jump,resulting a sudden increase in γ(T) following Eq. (17):γ(T)=θ₀(T)+β(T)j_(dc). In the mean time, the AC component may also havea sudden jump. In the calculation, the temperature T just before thesudden current increase can be used to calculate both the DC and the ACcurrent.

When the power system operates normally, the current in the conductor isa perfect sinusoidal function and the harmonics detected by the currentsensor follow Eqs. (22)-(25). However, when the system operatesabnormally, such relationship will break down. Therefore, the harmonicsof the detected signal can be analyzed to obtain the waveforminformation of the conductor current. Of cause, the instant waveform ofthe conductor current can be obtained with Eq. (20) without Fouriertransform.

FIG. 1 and FIG. 4 show examples where at least 3 fibers are used toconnect the signal processing unit containing the light source and thePD, and the sensor head which is free of electronic components andoptical detectors. It is beneficial to reduce the number of fibers forreducing the cost and the wiring complexity of the system duringinstallation. This can be accomplished by, for example, using an opticalreflection design in the current sensor head to reflect the probe lightto retrace its own path in generating the returned light towards thebase station for optical sensing.

Such a current sensor based on optical sensing with the above opticalreflection design in the current sensor head can include a sensor basestation including a light source that produces probe light, a firstoptical detector that receives a portion of the probe light of the lightsource to monitor power fluctuations of the light source and a secondoptical detector that detects light for sensing a current; an outputfiber line having a first fiber line terminal coupled to the sensor basestation to receive the probe light from the light source and to directthe received probe light to a second fiber line terminal of the outputfiber line away from the sensor base station; and an optical currentsensor head coupled to the second fiber line terminal of the outputfiber line to receive the probe light. The optical current sensor headis configured to include an input optical polarizer to filter the probelight to produce a polarized beam, a polarization beam splitter thatselectively outputs a first part of the polarized beam in a firstpolarization, a Faraday material located to receive and transmit thefirst part of the polarized beam in the first polarization as a modifiedoptical beam, a polarizer to transmit the modified optical beam and amirror to reflect the modified optical beam back to the polarizer, theFaraday material and the PBS which outputs the reflected modifiedoptical beam as an output beam separated from the probe light receivedby the optical current sensor head. The current sensor based on opticalsensing includes a return fiber line having a first fiber line terminalcoupled to the optical current sensor head to receive the output beam todeliver the output beam from the optical current sensor to the secondoptical detector in the sensor base station. The optical current sensorhead is located near or at a current-carrying conductor so that amagnetic field associated with the current is present at the Faradaymaterial and the second optical detector detects the output beam todetermine a magnitude of the current.

FIG. 9 discloses a first embodiment of a reflective current sensor head,in which the polarizer is oriented 45 degrees from the PBS passing axisso that the reflected light from the mirror is split 50% by the PBS intotwo separate fibers at zero magnetic field. At the signal processingside, a circulator or a coupler can be used to separate to forward andbackward going light of the first fiber. Fiber 1 can be a polarizationmaintaining fiber (PM), a single mode fiber (SM), or a multimode fiber(MM). If a more expensive polarization maintaining (PM) fiber is used, alight source with high DOP can be used and the polarization axis must bealigned with the slow (or fast) axis of the PM fiber. For the case ofusing a low DOP source, there is no requirement of the orientation ofthe PBS with respect to the input light. On the other hand, for the caseof PM fiber, the PBS's passing axis should be aligned with the slow (orfast) axis of the PM fiber.

FIG. 10 discloses a second embodiment of a reflective current sensorhead with an integrated temperature sensing capability. The PBS splits acertain percentage of light into the temperature sensing branch, whichconsists of a permanent Faraday rotator, a reflecting prism or mirror,and a collimator (collimator 3), and a fiber to sending temperaturerelated information to the remote signal processing unit. When SM or MMfiber is used as Fiber 1, low DOP source should be used and the PBSsplit 50% into the temperature sensing branch. When PM fiber is used asfiber 1, the slow axis of the PM fiber is aligned x° to the passing axisof the PBS to split a certain percentage of the incoming light into thetemperature sensing branch.

FIG. 11 illustrates a 3^(rd) embodiment of a reflective current sensor.The polarizer is oriented 45 degrees from the Wollaston prism passingaxis so that the reflected light is split 50% by the prism into twoseparate fibers at zero magnetic field. If PM fiber is used, the slowaxis (or fast axis) should be aligned with the passing axis of theWollaston prism. If SM or MM fiber is used, low DOP light source must beused to minimize the polarization sensitivity of the sensor system.

FIG. 12 illustrates a 4^(th) embodiment of a reflective current sensorhead with an integrated temperature sensor. A permanent Faraday rotatoris placed before the current sensing Faraday rotator with a rotationangle of x° at room temperature and is shielded from magnetic field. Thepolarizer is oriented 45°+x° to allow equal power splitting of thereflected light into the two fibers. When the temperature changes, thepower difference between the two fibers changes and such a change can beused to sense the temperature, similar the situation of FIG. 8.

FIG. 13 illustrates a current sensing system for simultaneouslymonitoring currents in three conductors in a 3-phase power system. Atemperature monitoring channel is also included to monitor theinstantaneous temperature to compensate the temperature dependence ofthe Verdet constant of the Faraday rotators used in the current sensingheads. In particular, the Verdet constant at different temperatures arestored in a look-up table of the digital circuit. When a temperature isobtained from the temperature sensor, the corresponding Verdet constantis located in the look-up table, which will be used for the electricalcurrent calculation. Note that a single light source is shared by foursensing channels to reduce the total cost.

While this patent document contains many specifics, these should not beconstrued as limitations on the scope of any invention or of what may beclaimed, but rather as descriptions of features that may be specific toparticular embodiments of particular inventions. Certain features thatare described in this patent document in the context of separateembodiments can also be implemented in combination in a singleembodiment. Conversely, various features that are described in thecontext of a single embodiment can also be implemented in multipleembodiments separately or in any suitable subcombination. Moreover,although features may be described above as acting in certaincombinations and even initially claimed as such, one or more featuresfrom a claimed combination can in some cases be excised from thecombination, and the claimed combination may be directed to asubcombination or variation of a subcombination. Similarly, whileoperations are depicted in the drawings in a particular order, thisshould not be understood as requiring that such operations be performedin the particular order shown or in sequential order, or that allillustrated operations be performed, to achieve desirable results.Moreover, the separation of various system components in the embodimentsdescribed in this patent document should not be understood as requiringsuch separation in all embodiments.

Only a few implementations and examples are described and otherimplementations, enhancements and variations can be made based on whatis described and illustrated in this patent document and attachedappendices.

What is claimed is:
 1. A current and temperature sensor based on opticalsensing, comprising: a sensor base station including a light source thatproduces probe light and an optical detection unit; an output fiber linehaving a first fiber line terminal coupled to the sensor base station toreceive the probe light from the light source and to direct the receivedprobe light to a second fiber line terminal of the output fiber lineaway from the sensor base station; an optical sensor head coupled to thesecond fiber line terminal of the output fiber line to receive the probelight and configured to include an input optical polarizer to filter theprobe light to produce a polarized input beam, a first Faraday materiallocated to receive and transmit the polarized input beam as a firstmodified optical beam and a second Faraday material to receive andtransmit the first modified optical beam as a second modified opticalbeam, and an optical polarization separation device that receives thesecond modified optical beam from the second Faraday material and splitsthe second modified optical beam into first and second beams in twodifferent polarizations along first and second optical paths,respectively, wherein the first Faraday material is configured toprovide a fixed change in polarization dependent on temperature and thesecond Faraday material is configured to provide a change inpolarization dependent on a magnetic field associated with analternating current (AC) carrying conductor; a first return fiber linehaving a first fiber line terminal coupled to the optical sensor head toreceive the first beam and a second fiber line terminal coupled to theoptical detection unit of the sensor base station to deliver the firstbeam from the optical sensor to the optical detection unit; and a secondreturn fiber line having a first fiber line terminal coupled to theoptical sensor head to receive the second beam and a second fiber lineterminal coupled to the optical detection unit of the sensor basestation to deliver the second beam from the optical sensor to theoptical detection unit, wherein the optical sensor head is located in aspace at a temperature so that a direct current (DC) portion of a changein polarization due to the first Faraday material is associated with thetemperature and the optical detection unit detects the two optical beamsto determine the temperature, and wherein the optical sensor head islocated near or at the alternating current carrying conductor so thatthe magnetic field associated with the alternating current is present atthe second Faraday material and the optical detection unit detects thetwo optical beams to determine a magnitude of the alternating current.2. The current and temperature sensor of claim 1, wherein the firstFaraday material is replaced with a temperature sensitive polarizationmaterial.
 3. The current and temperature sensor of claim 2, wherein thetemperature sensitive polarization material is a waveplate.
 4. Thecurrent and temperature sensor of claim 1, wherein the first Faradaymaterial is rotated during an assembly of the current and temperaturesensor to cause zero degrees of polarization rotation at a standard roomtemperature.
 5. The current and temperature sensor of claim 1, wherein apolarization rotation of the first Faraday material may be approximatedas a linear function of the difference between a current temperature anda standard room temperature.
 6. The current and temperature sensor ofclaim 1, wherein a polarization rotation of the first Faraday materialmay be approximated as a polynomial function of a difference between acurrent temperature and a standard room temperature.
 7. The current andtemperature sensor of claim 1, wherein the optical polarizationseparation device includes a Wollaston prism.
 8. The current andtemperature sensor of claim 1, wherein the output fiber line includes apolarization maintaining fiber segment.
 9. The current and temperaturesensor of claim 1, wherein the output fiber line includes a single modefiber segment.
 10. The current and temperature sensor of claim 1,wherein the output fiber line includes a multimode fiber segment.
 11. Acurrent and temperature sensor, comprising: a sensor base stationincluding a light source that produces probe light and an opticaldetection unit; an output fiber line having a first fiber line terminalcoupled to the sensor base station to receive the probe light from thelight source and to direct the received probe light to a second fiberline terminal of the output fiber line away from the sensor basestation; an optical sensor head coupled to the second fiber lineterminal of the output fiber line to receive the probe light, theoptical sensor head including: an optical beam splitter to split theprobe light into a current sensing beam and a temperature sensing beam,a first Faraday material located to receive and transmit the currentsensing beam as a first modified optical beam, wherein the first Faradaymaterial is located near or at a current carrying conductor so that amagnetic field associated with the current is present at the firstFaraday material, an optical polarization separation device thatreceives the first modified optical beam from the first Faraday materialand splits the first modified optical beam into a first polarization anda second polarization along first and second optical paths, wherein theoptical detection unit detects the first and second polarizations todetermine a magnitude of the current, a second Faraday material locatedto receive and transmit the temperature sensing beam as a secondmodified optical beam, wherein the second Faraday material is located tosense a temperature, and wherein the second Faraday material is orientedwith respect to the first Faraday material to prevent the currentcarrying conductor from affecting a polarization rotation by the secondFaraday material due to the temperature, wherein the optical detectionunit detects the second modified optical beam to determine atemperature; a first return fiber line coupled between the opticalsensor head and the sensor base station to direct the first polarizationof the first modified beam out of the optical sensor head to the sensorbase station; a second return fiber line coupled between the opticalsensor head and the sensor base station to direct the secondpolarization of the first modified beam out of the optical sensor headto the sensor base station; and a third return fiber line coupledbetween the optical sensor head and the sensor base station to directthe second modified beam out of the optical sensor head to the sensorbase station, wherein the optical detection unit includes: a firstoptical detector that detects the first polarization and a secondoptical detector that detects the second polarization to producedetector outputs representative of the current and a third opticaldetector that detects the second modified beam to produce anotherdetector output representative of the temperature.
 12. The current andtemperature sensor of claim 11, wherein the second Faraday material isreplaced with a temperature sensitive polarization material.
 13. Thecurrent and temperature sensor of claim 12, wherein the temperaturesensitive polarization material is a waveplate.
 14. The current andtemperature sensor of claim 11, wherein the second Faraday material isrotated during an assembly of the current and temperature sensor tocause zero degrees of polarization rotation at a standard roomtemperature.
 15. The current and temperature sensor of claim 11, whereina polarization rotation of the second Faraday material may beapproximated as a linear function of the difference between a currenttemperature and a standard room temperature.
 16. The current andtemperature sensor of claim 11, wherein a polarization rotation of thesecond Faraday material may be approximated as a polynomial function ofthe difference between a current temperature and a standard roomtemperature.
 17. The current and temperature sensor of claim 11, whereinthe optical polarization separation device includes a Wollaston prism.18. The current and temperature sensor of claim 11, wherein the outputfiber line includes a polarization maintaining fiber segment.
 19. Thecurrent and temperature sensor of claim 11, wherein the output fiberline includes a single mode fiber segment.
 20. The current andtemperature sensor of claim 11, wherein the output fiber line includes amultimode fiber segment.